Abstract
An Australian research microsatellite, FedSat with a complement of four payloads was launched from Tanegashima, Japan on 14 December 2002 into a near-circular sun synchronous 10:30 LT polar orbit at an inclination of 98.7° and altitude 800 km. Scientific experiments include a triaxial fluxgate magnetometer with a frequency response up to 100 Hz and a GPS receiver to monitor total electron content (TEC) and provide a precise orbit determination. Communications experiments include a Ka-band transponder and a UHF packet data service. A high performance computer payload will test reconfigurable computing technology.
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© 2003 Springer Science+Business Media Dordrecht
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Fraser, B.J. (2003). The FedSat Microsatellite Mission. In: Chian, A.CL., et al. Advances in Space Environment Research. Springer, Dordrecht. https://doi.org/10.1007/978-94-007-1069-6_28
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DOI: https://doi.org/10.1007/978-94-007-1069-6_28
Publisher Name: Springer, Dordrecht
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